DELTA 1 R/B, 2661

Orbit data source: Space-Track

DELTA 1 R/B, 2661 is space debris in SSO originally from a launch on Thu, 26 Jan 1967 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
2661, 1967-006B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1967-01-26 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 DELTA 1 R/B
1 02661U 67006B   26305.70547366 -.00000041  00000-0  31938-4 0  9992
2 02661 101.9173  29.5121 0065197 144.8278  10.0556 12.68029285765582
Epoch: 2026-11-01T16:55Z
TLE epoch observation values (Epoch: 2026-11-01T16:55:52.924Z)
Latitude
24.43781°
Longitude
-79.97561°
Altitude
1,342.781 km
Speed
7.212 km/s
True Right ascension
14h 19m 57s
True Declination
24° 19' 06"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
03:02:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,438.141 km
Perigee altitude
1,336.881 km
Semi-major axis
7,765.648 km
Eccentricity
0.00652
Inclination
101.9173°
RAAN
29.5121°
Arg. of periapsis
144.8278°
True anomaly
10.1871°
Mean anomaly
10.0556°
Eccentric anomaly
10.12124°
Mean motion
3.17159 °/min
Orbital period
113.51 mins
BSTAR
0.000031938
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Other satellites on launch #6 in the year 1967 (1967-01-26 UTC)

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